Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664

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Author:
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 670

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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1032

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Author: American Institute of Aeronautics and Astronautics
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9781563472855
Category : Computational fluid dynamics
Languages : en
Pages : 0

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Book Description
This document defines a number of key terms, discusses fundamental concepts, and specifies general procedures for conducting verification and validation of computational fluid dynamics simulations. It's goal is to provide a foundation for the major issues and concepts in verification and validation. However, it does not recommend standards in these areas because a number of important issues are not yet resolved.

Author: Donald D. Baals
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 218

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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704

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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 712

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A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)

Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 706

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Author:
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ISBN:
Category : Science
Languages : en
Pages : 1142

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Author:
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ISBN:
Category : Air-supported structures
Languages : en
Pages : 24

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Book Description
A small-scale, instrumented research aircraft was flown to investigate the flight characteristics of inflatable wings. Ground tests measured the static structural characteristics of the wing at different inflation pressures, and these results compared favorably with analytical predictions. A research-quality instrumentation system was assembled, largely from commercial off-the-shelf components, and installed in the aircraft. Initial flight operations were conducted with a conventional rigid wing having the same dimensions as the inflatable wing. Subsequent flights were conducted with the inflatable wing. Research maneuvers were executed to identify the trim, aerodynamic performance, and longitudinal stability and control characteristics of the vehicle in its different wing configurations. For the angle-of-attack range spanned in this flight program.